Gas turbine engine thrust reverser control

Power plants – Reaction motor – Interrelated reaction motors

Patent

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Details

60 39091, 602262, 244110B, F02K 132

Patent

active

051671190

ABSTRACT:
A gas turbine engine is provided with a thrust reverser. In order to avoid inadvertent operation of the thrust reverser when the gas turbine engine is not running, a safety switch is provided on the engine at a position remote from the thrust reverser. The thrust reverser control system is arranged so that when the engine is not running the thrust reverser will only operate when the safety switch is being manually operated.

REFERENCES:
patent: 3040524 (1962-06-01), Kurti
patent: 4424669 (1984-01-01), Fage

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